Moisture Path Close-Out and Thermal Control System and Methods of Assembling Same

ABSTRACT

A moisture control assembly for use with a support beam extending through an insulation layer is provided. The insulation layer is positioned between an outer wall and an inner wall. The assembly includes: a moisture path close-out structure coupled to the insulation layer at an aperture defined through the insulation layer, the moisture path close-out structure including an opening substantially aligned with the aperture and configured to receive the support beam therethrough; and a coupling mechanism configured to secure the moisture path close-out structure to the support beam such that the moisture path close-out structure is partially pulled away from the insulation layer, the coupling mechanism and the moisture path close-out structure configured to direct liquid flow down and away from the support beam and along the insulation layer.

This application is a continuation of prior U.S. patent application Ser.No. 15/257,563, filed 6 Sep. 2016, the disclosures of which areincorporated by reference herein in their entirety.

FIELD

The present disclosure generally relates to the moisture control field.More particularly, the present disclosure relates to the field ofmoisture control in a vehicle.

BACKGROUND

In an aircraft, the outer skin is spaced from the walls and ceiling of apassenger cabin (or other compartment), and the gap is at leastpartially filled with an insulation layer or blanket. The insulationlayer is typically formed from a waterproof material. During a flight,liquid from moist air can condense against the skin and freeze duringcruise. During decent, this frozen liquid can thaw and drip back downtowards the cabin. Because the insulation blanket is waterproof, thecondensate can flow along the insulation blanket and drain into thebilge. However, at some locations, structures and/or supports canprotrude through the insulation blanket. For example, the supports thathold monuments and bins to the crown extend from the structure at theskin, through the insulation blanket, and into the cabin. The insulationblankets come with predefined holes for the supports to extend throughthe blanket. The holes are lined, and there may be a gap defined betweenthe inner surface of the hole and the support. When liquid thaws, it candrip down through the hole and into the cabin.

One previous attempt to fix this problem was to wrap the support in feltso the felt will absorb the condensate and allow the condensate toevaporate back into the air. However, the condensate may be more thanthe felt can absorb. Further, wrapping each support in felt can betime-consuming.

BRIEF SUMMARY

There is provided, a moisture control assembly for use with a supportextending through an insulation layer, the insulation layer positionedbetween an outer wall and the inner wall, the assembly comprising: amoisture path close-out structure coupled to the insulation layer at anaperture defined through the insulation layer, the moisture pathclose-out structure including an opening substantially aligned with theaperture and configured to receive the support therethrough; and, acoupling mechanism configured to secure the moisture path close-outstructure to the support such that the moisture path close-out structureis partially pulled away from the insulation layer, the couplingmechanism and the moisture path close-out structure configured to directliquid flow down and away from the support and along the outboardsurface insulation layer.

In an aspect, the coupling mechanism and moisture path close-outstructure are configured to restrict air flow through the aperture whenthe moisture path close-out structure is secured to the support andcoupled to the insulation layer.

In an aspect, the moisture path close-out structure is coupled to theinsulation layer facing the outer wall.

In an aspect, the coupling mechanism is configured to partially pull themoisture path close-out structure away from the insulation layer andtowards the outer wall, when the moisture path close-out structure issecured to the support.

In an aspect, the moisture path close-out structure is a patch placedover the insulation layer.

In an aspect, the coupling mechanism further comprises a flange,diverging towards the insulation layer, attached to or integral with thesupport.

In an aspect, the moisture path close-out structure is attached to aside of the flange facing the insulation layer.

In an aspect, the flange is reversibly attached to the support.

In an aspect, the coupling mechanism further comprises a plug configuredfor insertion into a flange cavity, securing the moisture path close-outstructure in the flange cavity between the flange and the plug.

In an aspect, the moisture path close-out structure is secured to theplug.

In an aspect, the moisture path close-out structure is secured to thesupport by at least one of compression fit and friction fit between theflange and the plug.

In an aspect, the coupling mechanism further comprises at least onefastener screw or tab or adhesive to attach the plug to the flange.

In an aspect, the moisture control assembly further comprises a fillerdisposed between the moisture path close-out structure and theinsulation layer.

In an aspect, the filler is configured to mechanically press the pluginto the flange cavity.

In an aspect, the moisture path close-out structure is reversiblysecured to the support.

In an aspect, the moisture path close-out structure is umbrella-shaped.

In an aspect, the moisture control assembly further comprises aninsulating material positioned between the support and at least one ofthe inner wall and outer wall.

In an aspect, the moisture control assembly further comprises aninsulating material wrapped around at least a portion of the support.

In an aspect, the support is constructed of a material of low thermalconductivity.

There is further provided, a method for assembling a moisture pathclose-out and thermal control system for use with a support extendingthrough an insulation layer, the insulation layer positioned between anouter wall and an inner wall, the method including: inserting thesupport through an aperture defined through the insulation layer and anopening defined through a moisture path close-out structure, themoisture path close-out structure coupled to the insulation layer;coupling the moisture path close-out structure to the support using acoupling mechanism; and, pulling a portion of the moisture pathclose-out structure away from the insulation layer such that thecoupling mechanism and the moisture path close-out structure areconfigured to direct liquid flow down the support away from the supportand along the insulation layer.

In an aspect, the coupling comprises securing the moisture pathclose-out structure between a flange located on the support and a pluginserted therein.

Unless otherwise defined, all technical and/or scientific terms usedherein have the same meaning as commonly understood by one of ordinaryskill in the art to which the disclosed aspects pertain. Althoughmethods and materials similar or equivalent to those described hereincan be used in the practice or testing of aspects, exemplary methodsand/or materials are described below. In case of conflict, the patentspecification, including definitions, will control.

In addition, the components, materials, methods, and examples areillustrative only and are not intended to be necessarily limiting.

Implementation of the method and/or system of aspects of the disclosedaspects can involve performing or completing selected tasks manually,automatically, or a combination thereof. Moreover, according to actualinstrumentation and equipment of aspects of the method and/or system ofthe application, several selected tasks could be implemented byhardware, by software or by firmware or by any combination thereof,using for instance an operating system.

BRIEF DESCRIPTION OF THE DRAWINGS

Some aspects are herein described, by way of example only, withreference to the accompanying drawings and/or images. With specificreference now to the drawings in detail, it is stressed that theparticulars shown are by way of example, and not necessarily to scale,and are for purposes of illustrative discussion of the aspects:

FIG. 1 is a schematic diagram of an aircraft;

FIG. 2 is an exemplary cross-sectional, schematic view of an aircraft;

FIG. 3 is an exemplary block diagram of a moisture path close-out andthermal control system;

FIG. 4 is an exemplary side, partial cross-sectional view of a portionof a moisture path close-out and thermal control system;

FIG. 5 is a top view of a portion of a moisture path close-out andthermal control system;

FIG. 6 is a side view of a support beam with an insulating layer; and,

FIG. 7 is a flowchart of a method for assembling a moisture controlassembly.

DESCRIPTION Generally

The present disclosure generally relates to the moisture control field.More particularly, the present disclosure relates to the field ofmoisture control in a vehicle.

FIGS. 1-2 illustrate moisture flow in an exemplary aircraft, while FIGS.3-6 show an exemplary moisture path close-out and thermal control systemfor preventing or at least minimizing moisture flow into an inner cabinportion of the aircraft, according to some aspects of the disclosure.FIG. 1 shows an aircraft 100 that includes a nose 110, wings 120, afuselage 130, and a tail 140. FIG. 1 also illustrates a downward arrow150 indicating the expected direction in which the force of gravity willpull objects, such as liquid water, onboard an aircraft 100 in a nominaloperational profile.

FIG. 2 is a cross-sectional, schematic view of the aircraft 100indicated by view arrows 2 in FIG. 1. FIG. 2 illustrates a portion ofthe aircraft fuselage 130, simplified for easier understanding of thisDescription. The fuselage 130 includes floor 204, ceiling 206, andaesthetic fascia walls 208 which define the cabin 202, where the ceiling206 and/or aesthetic fascia walls 208 represent an “inner wall” of theaircraft for the purposes of this Description. Passengers in theaircraft 100 may congregate in seats 210 of the cabin 202 during flight.FIG. 2 illustrates that, inside of the fuselage 130 (e.g. in cabin 202),respiration and other sources of water cause moisture 220 to enter orform in the air in the cabin 202. For example, warm exhaled air includesmoisture 220 and rises upward through luggage compartments 212. Some ofthis warm and moist air rises through the ceiling 206. Furthermore, somewarm air continues to rise upward through an insulation layer 214 (orinsulation blanket) into a space 240 between the insulation layer 214and an outer wall 216 of the aircraft, also known as the aircraft skin.The insulation layer 214 includes an inboard surface 214 a and anoutboard surface 214 b as shown in FIG. 4. Also as shown in FIG. 4, anaperture 215 extends through the insulation layer 214, including throughthe inboard surface 214 a and the outboard surface 214 b.

Referring again to FIG. 2, as the skin 216 is cooled by the outside airat high altitude during flight, the temperature of the skin 216eventually decreases to a temperature below the freezing temperature ofwater. This cooling causes moisture 220 (e.g., water) to condense out ofthe air in the space 240 and freeze onto the inner surface of the skin216 as ice 218. As the aircraft changes to a lower altitude and/orcommences descent for landing and the temperature increases, the ice 218begins to melt causing water droplets 230 to travel through the space240 towards the bottom 250 of the fuselage 130, drawn by gravitationalforce 150. Some water droplets 230 enter gaps in the insulation layer214, particularly where support beams 222 pass through apertures 215within the insulation layer 214, and drip into the cabin 202, sometimeson passengers. The size of the space 240 has been exaggerated somewhatin FIG. 2 in order to more clearly show the details of the structure.Support beams 222 are often used for attaching aircraft components 224such as luggage compartments 212, the ceiling 206, ducting, equipment,and racks, as examples. For simplicity, common aircraft load bearingcomponents such as stringers and/or frame members are not shown, but itshould be understood that in some aspects, support beams 222 attachvarious aircraft components to stringers and/or frame members, and notdirectly to the outer wall 216 of the aircraft 100.

FIG. 3 is an exemplary block diagram of a moisture path close-out andthermal control system 300 (also referred to as a “moisture controlsystem” or a “moisture control assembly”), in an aspect of thedisclosure. In some aspects of the disclosure, a moisture path close-outstructure 302 is provided to the system 300 at a location vulnerable tomoisture leakage into the cabin 202, for example at the juncture betweena support beam 222 and the insulation layer 214 where typically there isa small gap. An umbrella-shaped structure 402, shown and described inmore detail with respect to FIGS. 4-5, is provided to the system 300 asthe moisture path close-out structure 302, in an aspect of thedisclosure. It should be understood that the umbrella-shaped structure402 is by way of example only, and that other functionally equivalentstructures could be used to prevent moisture from seeping into thejunction between the insulation layer 214 and the support beam 222. Inan aspect of the disclosure, the moisture path close-out structure isgenerally umbrella shaped at the top, but has a different shape (forexample ovoid, square, irregular, rectangular, multi-sided) at thebottom, depending on the available surface area near the aperture 215sought to be closed. The moisture path close-out structure 302 includesan opening, such as an opening 414 shown in FIG. 4. The openingsubstantially aligns with the aperture 215 through the insulation layer214 and receives at least a portion of the support beam 222therethrough.

In an aspect of the disclosure, the moisture path close-out structure302 also substantially, or even prevents, airflow between the cabin 202and the space 240 through the junction between the insulation layer 214and the support beam 222. For example, the moisture path close-outstructure 302 is constructed of an air impermeable material, such asexisting insulation blanket cover materials (such as BMS8-380 Type 4(Halar)—˜1 perm, BMS8-380 Type 3 (MPEEK)—˜0.5 perm, BMS8-380 Type 2(PEKK)—˜4 perm) and/or similar low permeable lightweight fabric. In anaspect, any material that is waterproof and can pass flammability, smokeand toxicity testing could be used. By blocking the airflow from thecabin 202, the moisture 220 from the cabin 202 is prevented fromentering the space 240 and condensing and freezing on the skin 216 inthe first place.

A coupling mechanism 304 is used to couple the moisture path close-outstructure 302 to the support beam 222 such that moisture flowing downthe support beam 222 cannot penetrate the coupling and must flow fromthe support beam 222 onto the moisture path close-out structure 302 andtowards the insulation layer 214 (shown and described in more detailwith respect to FIG. 4), where the moisture will eventually end up atthe bottom 250 of the aircraft fuselage 130. In some aspects of thedisclosure, the coupling mechanism 304 is an integral part of thesupport beam 222, optionally resulting from the support beam 222 beingmanufactured with the coupling mechanism 304 in the same manufacturingprocess. In some aspects, the coupling mechanism 304 is separate fromthe support beam 222 and is attached at some point prior to or as partof moisture path close-out and thermal control system installation. Sucha configuration is useful for retro-fitting support beams which havealready been manufactured/installed without the coupling mechanism 304,for example.

In some aspects, the coupling mechanism 304 couples the moistureclose-out structure 302 to the support beam 222 usingpressure/compression, adhesive, fasteners, tabs, screws and/or nails,stitching, wrapping, hook and pile fastener, zip-tie, threading (like ascrew), an external pressure exerting device (such as described withrespect to FIG. 4), and/or other device and/or method functionallysufficient to secure the moisture close-out structure 302 to the supportbeam 222 in a moisture impermeable manner.

In some aspects of the disclosure and as described in more detail below,a support beam 306, such as the support beam 222, is provided to system300 which is configured to assist with temperature control, which has aneffect on moisture control.

Umbrella-Shaped Moisture Path Close-Out Aspect

FIG. 4 is an exemplary side, partial cross-sectional view of a portionof a moisture path close-out and thermal control system 300 using anumbrella-shaped moisture close-out structure 302 as the moistureclose-out structure 302. The umbrella-shaped structure 402 includes anopening 414. The opening 414 substantially aligns with the aperture 215through the insulation layer 214 and receives at least a portion of thesupport beam 222 therethrough. In an aspect, the support beam 222 passesthrough the aperture 215 in the insulation layer 214 and the opening 414in the umbrella-shaped structure 402 and connects on an outboard side ofthe system 300 (with respect to the insulation layer 214) and on aninboard side (with respect to the insulation layer 214) to a portion ofthe inner wall of the aircraft 100 and/or aircraft components 224. In anaspect of the disclosure, the coupling mechanism 304 includes afrusto-conical shaped flange 404 through which passes the support beam222 and/or which is attached or integral to the support beam 222. Itshould be noted that in this example, the flange 404 is frusto-conicalin shape to match the general shape of the umbrella-shaped structure402; in other examples, where the moisture path close-out structure 302is another shape (i.e. not conical), the coupling mechanism 304 might beshaped differently. The flange 404 is configured to be reversiblyattached to the support beam 222, in some aspects.

The umbrella-shaped structure 402 is positioned with respect to theflange 404 such that droplets 230 flow down the support beam 222, flowover the flange 404 and over, but not through, the coupling between theflange 404 and the umbrella-shaped structure 402 and onward onto theinsulation layer 214, where it continues around on the water-proofinsulation layer 214 to the bottom 250 of the fuselage 130 (due togravitational force 150). In an aspect of the disclosure, this meansthat the upper end of the umbrella-shaped structure 402 is positionedwithin a flange cavity 408 of the flange 404 and on the side of theinsulation layer 214, such that at least a portion of the flange 404overlays the top of umbrella-shaped structure 402.

In an aspect, the flange 404 is located on the support beam 222 suchthat when the umbrella-shaped structure 402 is coupled to it, the upperend of the umbrella-shaped structure 402 is higher than the insulationlayer 214, providing a downward slope to the umbrella-shaped structure402 from the support beam 222 towards the insulation layer 214. In anaspect, the distance between the flange 404 and the insulation layer 214depends on the insulation blanket used and the angle of the support beam222. In an aspect, the material of the umbrella-shaped structure 402 isconfigured to be slack enough to allow for movement of the support beam222 without imparting a load on the material or insulation layer 214. Insome aspects, the coupling between the umbrella-shaped structure 402 andthe flange 404 pulls the umbrella-shaped structure 402 in an outboarddirection and away from the insulation layer 214 to create a slope.

In an aspect of the disclosure, a plug 406 is also placed around thesupport beam 222, but shaped to fit within the flange cavity 408 andpress the umbrella-shaped structure into the flange 404, therebysecuring the umbrella-shaped structure 402 between the flange 404 andthe plug 406. In some aspects, the umbrella-shaped structure 402 issecured to the plug 406 additionally or alternatively to being securedto the flange 404. In some aspects, the plug 406 is compressible (andlarger in diameter than the flange cavity 408) such that when the plug406 is pushed up into the flange cavity 408 of the flange 404, the plug406 compresses and secures the umbrella-shaped structure 402 via acompression fit and/or friction fit of the plug 406 within the flange404. In some aspects, the umbrella-shaped structure 402 is secured tothe plug 406 and/or the plug 406 is secured within the flange cavity 408using adhesive, fasteners, tabs, screws and/or nails, stitching,wrapping, hook and pile fastener, zip-tie, threading (like a screw), anexternal pressure exerting device (such as described with respect toFIG. 4), and/or other device and/or method functionally sufficient tosecure in a moisture impermeable manner. The umbrella-shaped structure402 is reversibly attached to the support beam 222, in some aspects.

In an aspect, the volume 412 between the umbrella-shaped structure 402and the insulation layer 214 is filled with a material/filler 410 (shownpartially in FIG. 4), for example, to prevent condensation fromcollecting in the volume 412 and/or to assist with mechanically holdingthe plug 406 in the flange cavity 408 by filling the volume 412 to anextent that the plug 406 is mechanically pushed into the flange cavity408.

It should be understood that the view of FIG. 4 is of a single supportbeam 222 with a moisture path close-out and/or thermal control system300 in place, and that similar configurations are optionally repeated atother support beams in the aircraft 100 where the system 300 would be ofbenefit for reducing precipitation of liquid moisture in the cabin 202.In some aspects, the aircraft 100 is configured with systems 300 on someor all support beams, which are located at or above where the width ofthe fuselage 130 is at its greatest from the cross-sectional perspectiveof FIG. 2.

FIG. 5 is a top view (from an outboard perspective looking inboard) of aportion of a moisture path close-out and thermal control system 300,including an umbrella-shaped structure 402 located within a flange 404.In an aspect, both the umbrella-shaped structure 402 and the flange 404are positioned around the support beam 222. In some aspects of thedisclosure, the umbrella-shaped structure 402 is fastened to theinsulation layer 214 at least with a first seam 502 and optionally, withone or more additional seams 504 to prevent moisture from penetratingthe junction between the umbrella-shaped structure 402 and theinsulation layer 214. In an aspect of the disclosure, the seams 502, 504are joined in a water impermeable fashion using an adhesive, stitching,and/or any of the other securing methods described herein and/oravailable in the art. In an aspect, and as shown in FIG. 5, the materialof the umbrella-shaped structure 402 does not need to completely coverthe surface of the insulation layer 214 because the insulation layer 214is already typically waterproof and the extra material would addunnecessary weight. In an aspect, the insulation layer 214 would includethe umbrella-shaped structure 402 as a patch coupled over a predefinedhole/aperture 215 through the insulation layer 214.

An access seam 506 is optionally provided to the umbrella-shapedstructure 402, for example to allow access through the system 300,either from inboard going outboard, or vice versa, for example foraccess during installation of the system 300. In an aspect, the accessseam 506 is water/moisture impermeable when closed. In some aspects, theaccess seam is water and vapor proof, using for example a water andvapor impermeable zipper and/or a hook and loop seam.

It should be understood that while the support beam 222 is shown asbeing circular in shape, the support beam 222 could be any shape andwhere the moisture path close-out structure 302 and the couplingmechanism 304 are configured to match that shape in order to effectivelyrender the junction between the support beam 222 and the insulationlayer 214 water impermeable, particularly from the outboard towardsinboard direction.

Temperature Control Support Beam Aspect

In some aspects, temperature control is utilized to maintain the supportbeam 222 above the dew point, at least in areas inboard of the moisturepath close-out structure 302 and/or the insulation layer 214, tominimize condensation. FIG. 6 is a side view of a support beam 222 withan insulating layer 602 positioned between the support beam 222 and theouter wall 216 (or wherever outboard of the insulation layer 214 thesupport beam 222 attaches) of the aircraft 100, in an aspect of thedisclosure. In an aspect, the insulating layer 602 is used to controlthe temperature of the support beam 222 by limiting the direct heattransfer path between the cold outer wall 216 (at altitude) and thesupport beam 222, ideally reducing condensation of moisture 220 presentin the space 240. Alternatively or additionally, an insulating layer issimilarly positioned on the inboard side of the support beam facing theinner wall (or wherever inboard of the insulation layer 214 the supportbeam 222 attaches). In an aspect, the insulating layer 602 is secured tothe outer wall 216 using any of the methods described herein and/orknown to those skilled in the art.

In an aspect, the support beam 222 is insulated over its entire length,for example, being coated with an insulating material and/or beingwrapped in a layer of insulation and/or being constructed of a materialwhich has a lower thermal conductivity relative to conventional aircraftconstruction materials.

Method of Assembly Aspect

FIG. 7 is a flowchart of a method (700) for assembling a moisture pathclose-out and thermal control system 300. In an aspect, the support beam222 is inserted (702) through an aperture 215 defined through theinsulation layer 214 and an opening defined through the moisture pathclose-out structure 302. In some aspects, the moisture path close-outstructure 302 is previously coupled to the insulation layer 214, forexample, during manufacture of the insulation layer 214. The moisturepath close-out structure 302 is coupled (704) to the support beam 222 bythe coupling mechanism 304 such that a portion of the moisture pathclose-out structure 302 is pulled (706) away from the insulation layer214 to impart a slope to the moisture path close-out structure 302directing liquid moisture flow down from the support beam 222 andtowards the insulation layer 214. In an aspect, the coupling (704) isachieved by securing the moisture path close-out structure 302 betweenthe flange 404 and the plug 406. In an aspect, the moisture pathclose-out structure 302 is the umbrella-shaped structure 402 describedelsewhere herein. In an aspect, the coupling mechanism 304 is attached(708) to the support beam 222 prior to coupling (704) the moisture pathclose-out structure 302 to the support beam 222, for example, where thesupport beam 222 is being retro-fitted to accept the moisture pathclose-out and thermal control system 300.

The terms “comprises”, “comprising”, “includes”, “including”, “having”and their conjugates mean “including but not limited to”.

As used herein, the singular form “a”, “an”, and “the” include pluralreferences unless the context clearly dictates otherwise. For example,the term “a compound” or “at least one compound” may include a pluralityof compounds, including mixtures thereof.

Throughout this application, various aspects or features may bepresented in a range format. It should be understood that thedescription in range format is merely for convenience and brevity andshould not be construed as an inflexible limitation on the scope of theapplication. Accordingly, the description of a range should beconsidered to have specifically disclosed all the possible subranges aswell as individual numerical values within that range. For example,description of a range such as from 1 to 6 should be considered to havespecifically disclosed subranges such as from 1 to 3, from 1 to 4, from1 to 5, from 2 to 4, from 2 to 6, from 3 to 6 etc., as well asindividual numbers within that range, for example, 1, 2, 3, 4, 5, and 6.This applies regardless of the breadth of the range.

It is appreciated that certain features of the application, which are,for clarity, described in the context of separate aspects, may also beprovided in combination in a single aspect. Conversely, various featuresof the application, which are, for brevity, described in the context ofa single aspect, may also be provided separately or in any suitablesubcombination or as suitable in any other described aspect of theapplication. Certain features described in the context of variousaspects are not to be considered essential features of those aspects,unless the aspect is inoperative without those elements.

Although specific aspects are described in the application, it isevident that many alternatives, modifications and variations will beapparent to those skilled in the art. Accordingly, it is intended toembrace all such alternatives, modifications and variations that fallwithin the spirit and broad scope of the appended claims.

Citation or identification of any reference in this application shallnot be construed as an admission that such reference is available asprior art to the present application, however, to the extent that anycitation or reference in this application does not contradict what isstated herein, it is incorporated by reference. To the extent thatsection headings are used, they should not be construed as necessarilylimiting.

The variations and alternatives of the present disclosure relate to, butare not limited to, components and parts designed to be positioned onthe exterior or interior of objects including, without limitation,atmospheric and aerospace vehicles and other objects, and structuresdesigned for use in space or other upper-atmosphere environments suchas, for example, manned or unmanned vehicles and objects. Contemplatedobjects include, but are not limited to vehicles such as, for example,aircraft, spacecraft, satellites, rockets, missiles, bombs, ballisticetc. and therefore include manned and unmanned aircraft, spacecraft,terrestrial, non-terrestrial, and even surface and sub-surfacewater-borne vehicles and objects.

What is claimed is:
 1. A moisture control assembly to controlcondensation within a space formed between an insulation layer and anouter wall of an aircraft, the moisture control assembly comprising: asupport beam that extends through an aperture in the insulation layer,the support beam comprising a first end at the outer wall and a secondend on an opposing side of the insulation layer; an insulation layerpositioned between the first end of the support beam and the outer wall,the insulation layer configured to limit direct heat transfer betweenthe outer wall and the support beam; a moisture path close-out structurecoupled to the insulation layer at the aperture of the insulation layer,the moisture path close-out structure including an opening substantiallyaligned with the aperture and configured to receive the support beamtherethrough; and a coupling mechanism coupled to the support beam andthat extends over a portion of and is coupled to the moisture pathclose-out structure; the moisture path close-out structure and thecoupling mechanism together shaped to direct liquid flow down and awayfrom the support beam and along an outboard surface of the insulationlayer.
 2. The moisture control assembly of claim 1, wherein the couplingmechanism is directly coupled to the moisture path close-out structureand configured to pull the moisture path close-out structure away fromthe insulation layer.
 3. The moisture control assembly of claim 1,wherein the coupling mechanism further comprises a plug positionedbetween the moisture path close-out structure and the support beam at asection where the moisture path close-out structure and the couplingmechanism overlap to secure the moisture path close-out structurebetween the coupling mechanism and the plug.
 4. The moisture controlassembly of claim 1, further comprising an insulating material thatextends over a length of the support beam.
 5. The moisture controlassembly of claim 4, wherein the insulating material is a coating. 6.The moisture control assembly of claim 4, wherein the insulatingmaterial is a layer that is wrapped onto the support beam.
 7. A moisturecontrol assembly for use with a support beam extending through aninsulation layer, the assembly comprising: a moisture path close-outstructure coupled to the insulation layer at an aperture defined throughthe insulation layer, the moisture path close-out structure including anopening substantially aligned with the aperture and configured toreceive the support beam therethrough; and a coupling mechanism coupledto the support beam and that extends over a portion of the moisture pathclose-out structure, the coupling mechanism being directly coupled tothe moisture path close-out structure and configured to pull themoisture path close-out structure away from the insulation layer todirect liquid flow down and away from the support beam and along anoutboard surface of the insulation layer.
 8. The moisture controlassembly of claim 7, further comprising an insulating material thatextends over a length of the support beam to control a temperature ofthe support beam.
 9. The moisture control assembly of claim 8, whereinthe insulating material is a coating.
 10. The moisture control assemblyof claim 8, wherein the insulating material is a layer that is wrappedonto the support beam.
 11. The moisture control assembly of claim 7,further comprising an insulation layer positioned at an end of thesupport beam to limit direct heat transfer between the outer wall andthe support beam.
 12. The moisture control assembly of claim 7, furthercomprising a plug positioned between the moisture path close-outstructure and the support beam at a section where the moisture pathclose-out structure and the coupling mechanism overlap to secure themoisture path close-out structure between the coupling mechanism and theplug.
 13. The moisture control assembly of claim 7, wherein the moisturepath closeout structure diverges towards the insulation layer.
 14. Amethod of assembling a moisture path close-out for use with a supportbeam extending through an insulation layer, the method including:inserting the support beam through an aperture defined through theinsulation layer and an opening defined through a moisture pathclose-out structure, the moisture path close-out structure directlycoupled to the insulation layer; coupling the moisture path close-outstructure to the support beam using a coupling mechanism wherein thecoupling mechanism directly contacts the moisture path close-outstructure; and pulling a portion of the moisture path close-outstructure away from the insulation layer by the coupling mechanism toimpart a slope to the moisture path close-out structure.
 15. The methodof claim 14, further comprising coating the support beam with aninsulating material.
 16. The method of claim 14, further comprisingwrapping a layer of insulation around the support beam.
 17. The methodof claim 14, further comprising positioning a first insulating layerbetween an end of the support beam and a wall to limit direct heattransfer between the wall and the support beam.
 18. The method of claim14, further comprising positioning a second insulating layer on anopposing second end of the beam that is positioned away from the wall.19. The method of claim 17, further comprising securing the firstinsulating layer to the wall with an outer side of the first insulatinglayer positioned against the wall and an inner side of the firstinsulating layer positioned against the support beam.
 20. The method ofclaim 15, further comprising coating the support beam with theinsulating material prior to inserting the support beam through anaperture defined through the insulation layer and an opening definedthrough a moisture path close-out structure.